
\begin{table}
\label{mesh_stats_Minimu}
\tiny
\begin{tabular}{llllllllllll}
Iter&Method&Nodes&NV&NC&OE&CE&JE&HE&RHS&$\epsilon_{\max}$&CPU(sec)\\ \hline \\
1&LGL-ST&80&322&247&747&746&89&0&59680&1.752e-03&8.020e+00\\
2&LGL-ST&90&362&277&70&71&55&0&6390&1.706e-03&6.890e+00\\
3&LGL-ST&100&402&307&28&29&28&0&2900&7.940e-04&4.810e+00\\
\hline
-&-&-&-&-&845&846&172&0&68970&-&1.972e+01\\
\end{tabular}
\newline \\ \emph{Key}: Iter=iteration number, NV=number of variables, NC=number of constraints, OE=objective evaluations,  	              CE = constraint evaluations, JE = Jacobian evaluations, HE = Hessian evaluations, RHS = ODE right hand side 		      evaluations, $\epsilon_{\max}$ = maximum relative ODE error, CPU(sec) = CPU time in seconds spent by nonlinear programming algorithm
\normalsize
\caption{Mesh refinement statistics: Minimum time to climb for a supersonic aircraft}
\end{table}